











|
 |
Characteristics:
| Height |
<800
mm |
Main
rotor diam. |
3
bladed, diam. 3000 mm |
| Gross
Weight, lbs |
32 |
Payload
Weight, lbs |
110 |
| Fuel
Capacity |
Max 25 liters.
Supplied with 2 x 5 ltr Kevlar |
Fuel
Type |
Gas
and oil mix (40:1) |
| Engine
Make |
ZDZ
160 cc |
Motor
output |
17
shaft hp (12.5 kw) |
| Structure |
Carbon,
kevlar |
|
| Guidance |
|
Navigation |
|
| Data
Link(s) |
|
Data
Rate(s) |
|
Performance:
| Duration,
hrs |
<2
(+ - payload) |
Range,
km |
<200 |
| Max
Speed, kts |
|
Stall
Speed, kts |
|
| Altitude,
mtr |
1500 |
|
| Takeoff
Means |
|
|
| Navigation |
|
|
| Landing
Means |
|
|
|
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